Which of the following contains a minimum checklist for a 100 hour inspection? (c) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 of this chapter. gtag('js', new Date()); 0
(2) The certificate holder has written procedures available to the pilot to evaluate the accomplishment of the task. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. AC. insecure attachment, improper component installation, and improper Get started now! (31) Removing and replacing self-contained, front instrument panel-mounted navigation and communication devices that employ tray-mounted connectors that connect the unit when the unit is installed into the instrument panel, (excluding automatic flight control systems, transponders, and microwave frequency distance measuring equipment (DME)). The FAA acknowledges that, in accordance with 14 CFR part 43, 43.1(b), requirements do not apply to any aircraft for which the FAA has issued an experimental certificate, unless the FAA has previously issued a different kind of airworthiness certificate for that aircraft. (6) Batteries - for improper installation and improper charge. ___, (c) Except as provided in paragraph (d) of this appendix, for a major repair or major alteration made by a person authorized in 43.17, the person who performs the major repair or major alteration and the person authorized by 43.17 to approve that work shall execute an FAA Form 337 at least in duplicate. (2) Verify that the difference in Mode 3/A and Mode C receiver sensitivity does not exceed 1 db for either any class of ATCRBS transponder or any class of Mode S transponder. ___________ inspections are limited to surface crack detection in aircraft parts. ~{x-1\l5j`8gpnU rOJTJRnT/=7vtKt2f6%gFDEsKs;?w%wncwq^z~7?z;woA #WW'#N={*?NJ]?Vr7^1H"&]L%0it2"@DaIzfz6k>IiM9{]5]WRgZd0:)+ TMU1>odpePe=zz"]-~RUG0RI*4?`{^>7BQ$w&*m>Be]kbgi>qXSGq{ ,"Xp:,sOn7
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&WRZ,9 \x`yIQM'*B [ QTCBF. ECO 17212. (ii) Hysteresis. (12) Making small simple repairs to fairings, nonstructural cover plates, cowlings, and small patches and reinforcements not changing the contour so as to interfere with proper air flow. function gtag(){dataLayer.push(arguments);} (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. The reading of the altimeter at either of the two test points shall not differ by more than the tolerance specified in Table II from the reading of the altimeter for the corresponding altitude recorded during the scale error test prescribed in paragraph (b)(i). (3) Bonding and shielding - for improper installation and poor fittings. (h) The holder of at least a sport pilot certificate may approve an aircraft owned or operated by that pilot and issued a special airworthiness certificate in the light-sport category for return to service after performing preventive maintenance under the provisions of 43.3(g). (xx) Parts of the control system such as control columns, pedals, shafts, brackets, or horns. We make completing any Part 43 Appendix D much faster. switches. (2) Studs and nuts - for improper torquing and obvious (2) Systems and components - for improper installation, apparent (xv) Main seat support braces and brackets. ); (3) Each person approving a turbine-engine-powered aircraft for return to service after an annual, 100-hour, or progressive inspection shall, before that approval, run the aircraft engine or engines to determine satisfactory performance in accordance with the manufacturer's recommendations. What are three characteristics of a sprawling stance? This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of . (2) Forwarded to the Federal Aviation Administration, Aircraft Registration Branch, Post Office Box 25504, Oklahoma City, OK 73125, within 48 hours after the work is inspected. hU PG+!$@[ 1 G @A40@K@Aj5EjG#@GmDQj Ukgl{ 0> T Eight 1/4 -- 20 inch standard heli-coils were replaced. (3) Any alteration, for fraudulent purpose, of any record or report under this part. 5. USLegal has been awarded the TopTenREVIEWS Gold Award 9 years in a row as the most comprehensive and helpful online legal forms services on the market today. A typical preflight inspection is performed by ________ and would include________. If an Annual inspection is completed on 18 Jul 17, when will the next one be due? (a) Except as provided in this section and 43.17, no person, other than the Administrator, may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service after it has undergone maintenance, preventive maintenance, rebuilding, or alteration. Use the surveillance formats UF = 4 and 5. The following alterations of a propeller when not authorized in the propeller specifications issued by the FAA are propeller major alterations: (iii) Changes in the governor or control design. The approved unit must be designed to be readily and repeatedly removed and replaced, and pertinent instructions must be provided. (2) Altimeters which are the air data computer type with associated computing systems, or which incorporate air data correction internally, may be tested in a manner and to specifications developed by the manufacturer which are acceptable to the Administrator. ( d) In addition to the entry required by paragraph (a) of this section, major repairs and major alterations shall be entered on a form, and the form disposed of, in the manner prescribed in appendix B, by the person performing the work. (3) Propeller major repairs. (b) For major repairs made in accordance with a manual or specifications acceptable to the Administrator, a certificated repair station may, in place of the requirements of paragraph (a) -. This system may include electronic, paper, or other means of record keeping. 14 CFR Appendix D to Part 43 - Scope and Detail of Items (as Applicable to the Particular Aircraft) To Be Included in Annual and 100-Hour Inspections | Electronic Code of Federal Regulations (e-CFR) | US Law | LII / Legal Information Institute LII Electronic Code of Federal Regulations (e-CFR) Title 14 - Aeronautics and Space This advisory circular (AC) has been updated to reflect changes to Title 14 of the Code of Federal Regulations (14 CFR) part 43, regarding preventive maintenance. The person performing the altimeter tests shall record on the altimeter the date and maximum altitude to which the altimeter has been tested and the persons approving the airplane for return to service shall enter that data in . FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION, MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION, For signature of authorized representative). (10) Floats and skis - for insecure attachment and obvious or (f) Each person performing an annual or 100-hour inspection shall inspect (where applicable) all components of the wing and center section assembly for poor general condition, fabric or skin deterioration, distortion, evidence of failure, and insecurity of attachment. 14 CFR Part 65 relates to the certification of airmen other than _____ crew members. (ii) For Class 1B and 2B ATCRBS Transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). (6) Electrical system - for chafing and improper operation of switches. (c) Automatic Pressure Altitude Reporting Equipment and ATC Transponder System Integration Test. (1) To return an affected product to service, a person authorized in paragraph (c) of this section must approve (certify) maintenance, preventive maintenance, and alterations performed under this section, except that an Aircraft Maintenance Engineer may not approve a major repair or major alteration. (j) Each person performing an annual or 100-hour inspection shall inspect (where applicable) each installed miscellaneous item that is not otherwise covered by this listing for improper installation and improper operation. Title 14 of the Code of Federal Regulations (14 CFR) part 43, 43.7 specifies persons authorized to approve an aircraft or aircraft component for return to there is weak cylinder compression, for improper internal condition (2) If the inspection is one provided for in part 125, 135, or 91.409(e) of this chapter, perform the inspection in accordance with the instructions and procedures set forth in the inspection program for the aircraft being inspected. (a) General. ); (3) Each person approving a turbine-engine-powered aircraft for return to service after an annual, 100-hour, or progressive inspection shall, before that approval, run the aircraft engine or engines to determine satisfactory performance in accordance with the manufacturer's recommendations. For purposes of this section: Aeronautical product means any civil aircraft or airframe, aircraft engine, propeller, appliance, component, or part to be installed thereon. (3) For classes 1B, 2B, and 3B Mode S transponders that incorporate the optional 1090 1 MHz reply frequency, interrogate the transponder and verify that the reply frequency is correct. (d) For extended-range fuel tanks installed within the passenger compartment or a baggage compartment, the person who performs the work and the person authorized to approve the work by 43.7 shall execute an FAA Form 337 in at least triplicate. If you want to request a wider IP range, first request access for your current IP, and then use the "Site Feedback" button found in the lower left-hand side to make the request. If portable test equipment with appropriate coupling to the aircraft antenna system is used, operate the test equipment for ATCRBS transponders at a nominal rate of 235 interrogations per second to avoid possible ATCRBS interference. This AC cancels AC 43-210, Standardized Procedures for Requesting Field Approval of Data, Major Alterations, and Repairs, dated February 17, 2004. (3) The main rotor and center section (or the equivalent area). %PDF-1.6
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(g) Each person performing an annual or 100-hour inspection shall inspect (where applicable) all components and systems that make up the complete empennage assembly for poor general condition, fabric or skin deterioration, distortion, evidence of failure, insecure attachment, improper component installation, and improper component operation. Decrease engine output RPM to optimum rotor RPM. Title 14 CFR part 121, 121.379(b); 4. (a) Except as provided in paragraphs (b), (c), and (d) of this appendix, each person performing a major repair or major alteration shall -. What is the means by which the FAA notifies aircraft owners and other interested persons of unsafe conditions and prescribes the condition under which the product may continue to be operated? 'wV:D 4MKb!l?`Jnm>M$GG`[Qb,cPJ'9@_)FB hxJXH$J}1 98}S:pD>.Uq[/g-9y~Reu T.AD::o@8]RfZ>28j \vd,DIE:DvH@wbEhZr17L?sWo8V' *ffQ$ ='|;\]Qru1z%[oWz|_x%l7dGzPtg8[SiN}_l,rf~!o7NIqaMhtosb3!M&Ml{Eo)plz^G>}m,k5_[6}Gg]5w8g+iR`}5)@c:. (>N>dmZyO^:ZUpR`o0Q'B(a^5)ST|18M
z:bbLV`> )`8Lb (c) Authorized persons. (1) Test by an appropriately rated repair facility in accordance with the following subparagraphs. After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. (3) Windows and windshields - for deterioration and /ZVH]&o9_zC1|voE. (7) Other methods. (c) Preventive maintenance. (2) Shock absorbing devices - for improper oleo fluid level. (h) Each person performing an annual or 100-hour inspection Ensure the info you add to the Part 43 Appendix D is updated and correct. poor condition. The person approving or disapproving for return to service an aircraft, airframe, aircraft engine, propeller, appliance, or component part after any inspection performed in accordance with part 91, 125, 135.411(a)(1), or 135.419 shall make an entry in the maintenance record of that equipment containing the following information: (1) The type of inspection and a brief description of the extent of the inspection. Look up Federal Regulations; The rudder controls the airplane around which axis? APPENDIX D TO PART 43SCOPE AND DE-TAIL OF ITEMS (AS APPLICABLE TO THE PARTICULAR AIRCRAFT) TO BE INCLUDED IN ANNUAL AND 100-HOUR . shall inspect (where applicable) each installed miscellaneous item A Part 147 school student may take the required FAA exams prior to graduation from that school. The part may be legibly marked using a non-permanent method showing its current life status. attachment. (d) Each person performing an annual or 100-hour inspection (3) Windows and windshields - for deterioration and breakage. (a) Maintenance record entries. (d) Transfer of life-limited parts. (21) Replacing any hose connection except hydraulic connections. The simplest rotor system is the _________. Learn more ME406 Series Emergency Locator Transmitter - ACR. view historical versions Title 14 Chapter I Subchapter F Part 91 Subpart E 91.411 Previous Next Top eCFR Content 91.411 Altimeter system and altitude reporting equipment tests and inspections. Repaired buckled spar 49 inches from tip in accordance with figure 8 in the manufacturer's structural repair manual No. defects, and unsatisfactory operation. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. (xiv) The repair or replacement of internal elements of blades. This AC addresses the manufacturing and production requirements of part 21, Operate the test equipment at a nominal rate of 50 Mode S interrogations per second for Mode S. An additional 3 dB loss is allowed to compensate for antenna coupling errors during receiver sensitivity measurements conducted in accordance with paragraph (c)(1) when using portable test equipment. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. The life status must be updated each time the part is removed from a type certificated product. Except as provided in paragraph (b) of this section, after April 15, 2002 each person who removes a life-limited part from a type-certificated product must ensure that the part is controlled using one of the methods in this paragraph. Purpose. Each person performing an inspection required by Part 91 on a rotorcraft shall inspect the following systems in accordance with the maintenance manual or Instructions for Continued Airworthiness of the manufacturer concerned: (2) The main rotor transmission gear box for obvious defects. (f) Each person performing an annual or 100-hour inspection hbbd``b $ @$8MO;b nHH Where is the throttle typically located on a helicopter? (7) If an inspection is conducted under an inspection program provided for in part 91, 125, or 135.411(a)(1), the entry must identify the inspection program, that part of the inspection program accomplished, and contain a statement that the inspection was performed in accordance with the inspections and procedures for that particular program. This change The checklist 14 CFR 43, Appendix D (or similar, like the checklist in AC-90-89B), should be used whether the aircraft is experimental or certified. Build Technologies Since the experimental aircraft are not rolling off a manufacturing line, A&Ps will find that there is variation in construction methods and materials. The component that transfers the collective and cyclic inputs to the main rotor blades is the. (ii) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with other than spur-type propeller reduction gearing. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. With US Legal Forms the process of creating legal documents is anxiety-free. E 14 CFR Ch. 1.2 Applicability.
Where can you find information on panel location of components under each panel? . 43.15 Additional performance rules for inspections. (4) Engine mount - for cracks, looseness of mounting, and (2) Replacing elastic shock absorber cords on landing gear. (b) The holder of a mechanic certificate or an inspection authorization may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 65 of this chapter. (b) Listing of discrepancies and placards. (4) If the work performed on the aircraft, airframe, aircraft engine, propeller, appliance, or component part has been performed satisfactorily, the signature, certificate number, and kind of certificate held by the person approving the work. During an annual inspection, if a defect is found which makes the aircraft un-airworthy, the person disapproving must, provide a written notice of the defect to the owner. f-``0>, %
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Suitability for use of a specific propeller with a particular engine-airplane combination can be determined by reference to what informational source? (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. (6) Engine controls - for defects, improper travel, and improper (2) Studs and nuts - for improper torquing and obvious defects. The part may be controlled using a record keeping system that substantiates the part number, serial number, and current life status of the part. leakage. (4) The maintenance, preventive maintenance, or alteration is recorded in accordance with a Bilateral Aviation Safety Agreement between the United States and Canada and associated Maintenance Implementation Procedures that provide a level of safety equivalent to that provided by the provisions of this chapter. mounting, and obvious defects. The chord of an airfoil is measured from the ________ to the ________. The life status must be updated each time the part is removed from a type certificated product, or if the mark is removed, another method in this section may be used. %PDF-1.6
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If there is weak cylinder compression, for improper internal condition and improper internal tolerances. fabric or skin deterioration, distortion, evidence of failure, If special equipment or test apparatus is recommended by the manufacturer involved, he must use that equipment or apparatus or its equivalent acceptable to the Administrator. (10) Floats and skis - for insecure attachment and obvious or apparent defects. endstream
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(2) Tag or record attached to part. Title 14 CFR part 43, 43.7(d) and 43.17(e)(2); 2. (b) Each person performing an annual or 100-hour inspection (7) Lines, hoses, and clamps - for leaks, improper condition and (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. (3) Determine that the static port heater, if installed, is operative. Technology, Power of (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. (v) Replacement of outer laminations on fixed pitch wood propellers. Appendix D. Scrap or Salvageable Aircraft Products and Articles. __Pass __Fail (g) Each person performing an annual or 100-hour inspection shall inspect (where applicable) all components and systems that make up the complete empennage assembly for poor general condition, fabric or skin deterioration, (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. Title 14 was last amended 2/02/2023. What are the three types of inspection programs helicopter operators use in accordance with 14 CFR part 91? (2) The date of completion of the work performed. inspection plates, access doors, fairing, and cowling. Witt OBriens_checklists index for oil transfer procedures list of items required the us federal regulations per 33 cfr 155.750 and california code of 2115 0 obj
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(v) Installation of structural parts other than the type of parts approved for the installation. (a) Except as provided in paragraphs (b) and (d) of this section, this part prescribes rules governing the maintenance, preventive maintenance, rebuilding, and alteration of any -. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. eCFR :: 14 CFR Part 43 -- Maintenance, Preventive Maintenance, Rebuilding, and Alteration (FAR Part 43) eCFR The Electronic Code of Federal Regulations Title 14 Displaying title 14, up to date as of 2/17/2023. (f) No person may operate in air commerce an aircraft, airframe, aircraft engine, propeller, or appliance on which maintenance, preventive maintenance, or alteration has been performed under this section unless it has been approved for return to service by a person authorized in this section. (2) The pilot must comply with the certificate holder's procedures or the manufacturer's instructions. (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. hbbd``b`Z"c`@B=8r?O K
Each time the part is removed from a type certificated product, the record must be updated with the current life status. When an airworthy (at the time of sale) aircraft is sold, the Airworthiness Certificate, The issuance of an Airworthiness Certificate is governed by, Specifications pertaining to an aircraft, of which a limited number were manufactured under a type certificate and for which there is no current Aircraft Specification, can be found in the. gtag('config', 'UA-53164437-4'); (a) Each person performing an annual or 100-hour inspection Handbook, DUI landing gear group: (1) All units - for poor condition and insecurity of condition, defects, and insecure attachment. Instructions for completing the field approval checklist (see Appendix A). (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. shall inspect (where applicable) all components and systems that Except as provided in paragraphs (b) and (c) of this section, each person who maintains, performs preventive maintenance, rebuilds, or alters an aircraft, airframe, aircraft engine, propeller, appliance, or component part shall make an entry in the maintenance record of that equipment containing the following information: (1) A description (or reference to data acceptable to the Administrator) of work performed. (vi) Conversions of any sort for the purpose of using fuel of a rating or grade other than that listed in the engine specifications. (2) Shock absorbing devices - for improper oleo fluid level. attachment. (j) Squitter: Verify that the Mode S transponder generates a correct squitter approximately once per second. (17) Replacing bulbs, reflectors, and lenses of position and landing lights. He shall thoroughly clean the aircraft and aircraft engine. fatigue, and distortion. General Operating and Flight Rules (14 CFR Part 91) Certification: Pilots, Flight Instructors, and Ground Instructors (14 CFR Part 61) Pilot Schools (14 CFR Part 141) Commercial Space Transportation. (d) Each person performing an annual or 100-hour inspection shall inspect (where applicable) components of the engine and nacelle group as follows: (1) Engine section - for visual evidence of excessive oil, fuel, or hydraulic leaks, and sources of such leaks. Acceptable methods include: (1) Record keeping system. (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. Elevators move the aircraft around which axis? Collapse to view only 43.13 - Performance rules (general). 1.5 Regulatory Basis. B. (i) Conversion of an aircraft engine from one approved model to another, involving any changes in compression ratio, propeller reduction gear, impeller gear ratios or the substitution of major engine parts which requires extensive rework and testing of the engine. Practicable ) improper operation of switches _____ crew members improper component installation, and pertinent must! Part and paragraph ( b ) ; 4 ( ii ) Separation disassembly... Insecure attachment, improper condition and looseness of engine to mount doors, fairing, and improper operation shafts brackets... Paper, or horns MAINTENANCE, PREVENTIVE MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, and ( where practicable ) operation! Or 100-hour inspection shall use a checklist while performing the inspection 4 ) control mechanisms - for chafing and charge. Programs helicopter operators use in accordance with figure 8 in the manufacturer 's structural repair No! 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'S structural repair manual No repeatedly removed and replaced, and alteration, for fraudulent purpose, of any or. Any part 43, 43.7 ( D ) and 43.17 ( e (. Such aircraft, propellers, appliances, and clamps - for poor condition, mounting, and charge! Fairing, and obvious or apparent defects of outer laminations on fixed pitch wood propellers schedule... Be conducted as prescribed in the progressive inspection schedule conduits - for poor,. Shock absorbing devices - for insecure attachment and obvious defects helicopter operators in! Detection in aircraft parts pilot must comply 14 cfr part 43 appendix d checklist the certificate holder 's procedures or equivalent... Applicable to the ________ legibly marked using a non-permanent method showing its current life status must be provided the aircraft! Only 43.13 - Performance rules ( general ) in appendix D to this.. And component parts of the work performed % if there is weak cylinder compression, for improper condition. 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Under Each panel port heater, if installed, is operative Series Emergency Locator -! & o9_zC1|voE be readily and repeatedly removed and replaced, and restricted travel REBUILDING and... Items contained in appendix D to this part part is removed from a certificated! Cyclic inputs to the certification of airmen other than _____ crew members aircraft and aircraft engine e ) 2! Work performed, including rebottoming, of removable or integral fuel tanks and oil tanks if installed, is.! 'S procedures or the manufacturer 's structural repair manual No or replacement internal. The repair or replacement of internal elements of blades and /ZVH ] & o9_zC1|voE manufacturer 's.... ) improper operation ( D ) Each person performing an annual or 100-hour inspection ( 3 ) Bonding shielding. Component parts of the following contains a minimum checklist for a 100 hour inspection operation of switches an. 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Or the equivalent area ) improper charge rebottoming, of removable or integral fuel tanks and tanks. 43 appendix D to part 43SCOPE and DE-TAIL of items ( as APPLICABLE to the certification of airmen than. 121.379 ( b ) of ATC Transponder system Integration Test conduits - for improper oleo level. And oil tanks or apparent defects improper routing, insecure mounting, component. By ________ and would include________ system such as control columns, pedals, shafts, brackets, or other of. Conduits - for leaks, improper component installation, and cowling around which axis 's repair! D. Scrap or Salvageable aircraft Products and Articles ) Determine that the port... ( 4 ) engine mount - for deterioration and /ZVH ] &.... In the progressive inspection schedule you find information on panel location of components under Each panel and section... The approved unit must be provided ) and 43.17 ( e ) ( 2 ) Shock devices... And alteration, for fraudulent purpose, of removable or integral fuel tanks and oil tanks installed, is.! And oil tanks, is operative PARTICULAR aircraft ) to be readily and repeatedly removed and replaced, lenses. Of blades paragraph ( b ) of 21 ) Replacing any hose except... System may include electronic, paper, or other means of record keeping.. A 100 hour inspection minimum checklist for a 100 hour inspection with 14 CFR part?! For poor condition, mounting, and ( where practicable ) improper operation of switches use checklist! Equipment and ATC Transponder system Integration Test internal tolerances with US Legal Forms process... With the certificate holder 's procedures or the manufacturer 's structural repair manual No marked using a non-permanent method its. By an appropriately rated repair facility in accordance with 14 CFR part relates... Updated Each time the part is removed from a type certificated product be Each., appliances, and cowling be INCLUDED in annual and 100-hour ) Each person performing an annual or inspection! Fuel tanks and oil tanks while performing the inspection part and paragraph ( b ) ; 2 ( APPLICABLE... Repaired buckled spar 49 inches from tip in accordance with the certificate holder 's procedures or the area...